Part-66 Module 11 Practice Questions - EASA Part-66 Module 11 - Aeroplane Aerodynamics, Structures And Systems Exam

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As airflow passes through a normal shock wave on the upper surface of a wing in transonic flight, the static pressure of the air:

Decreases and velocity increases Increases and velocity decreases to subsonic Remains constant while temperature falls Decreases while density falls

Correct Answer:

Increases and velocity decreases to subsonic

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